Nickel-Copper Alloy, Corrosion Resistant, Sheet, Strip, and Plate 67Ni - 30Cu Annealed
- Aerospace Material Specification
- AMS4544H
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Nickel, Sheet and Strip Low (0.02 max) Carbon Annealed |
| Aerospace Material Specification | Alloy, Corrosion-Resistant, Bars 20Cr - 35Ni - 35Co - 10Mo Vacuum Induction Plus Consumable Electrode Vacuum Remelted Solution Heat Treated for Work Strengthening |
| Aerospace Material Specification | Alloy, Corrosion and Heat-Resistant, Sheet, Strip and Plate 21Cr - 32.5Ni - 0.38Ti - 0.38Al - 45Fe Solution Heat Treated |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| [Unnamed Dataset 1] | ||
| [Unnamed Dataset 2] | ||
| Table 1 | Composition | |
| Table 2 | Tensile properties | |
| Table 3 | Hardness |
Issuing Committee
AMS F Corrosion Heat Resistant Alloys Committee
The committee of Corrosion and Heat Resistant Steels and Alloys and Specialty Steels and Alloys, AMS Committee F, will prepare, coordinate, and revise documents related to corrosion and heat resistant steels and alloys and specialty steels and alloys technology, such as stainless steels and nickel and base alloys, through the participation of metals suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace materials.